FIELD
[0001] The embodiments discussed herein are related to an optical frequency division multiplexer
and a polarization control method.
BACKGROUND
[0002] In future optical networks, such techniques may be requested in which optical signals
can be multiplexed in relay nodes and terminal station devices in optical networks,
or in the midway point of transmission lines, for example. For one of promising techniques
for multiplexing, an optical frequency division multiplexing technique is known. The
optical frequency division multiplexing technique is a method in which information
signals at different subcarrier frequencies are all-optically multiplexed on a carrier
light beam at a single wavelength for transmission.
[0003] In the case where typical signal multiplexing techniques are sorted, there is an
O/E/O method that implements signal multiplexing in which an optical signal (O) is
temporarily converted into an electrical signal (E), the electrical signal is multiplexed,
and the electrical signal is again converted into an optical signal (O). Moreover,
there is an all-optical signal multiplexing method that does not involve optoelectric
conversion into electrical signals.
[0004] The O/E/O method can adopt a multiplexing method such as time division multiplexing,
phase multiplexing, and frequency multiplexing, for example. However, processing time
becomes longer as the number of signals to be multiplexed is increased, and in addition
to that, loads are gathered on devices on the downstream side as the number of major
nodes is increased. Moreover, the use of electrical signal processing causes degraded
energy efficiency, and puts limitations on processing speed. Under the present circumstances,
a processing speed of a few tens GHz is the upper limit.
[0005] On the other hand, for the all-optical signal multiplexing method, a wavelength multiplexing
method is known, for example. In the wavelength multiplexing method, a plurality of
carrier light beams at different wavelengths is subjected to base band modulation,
and multiplexed and demultiplexed using an optical multiplexing and demultiplexing
filter. Therefore, in performing multiplexing at narrow wavelength (frequency) intervals,
considerably highly accurate wavelength control may be necessary at a transmitting
station and a wavelength demultiplexer because the multiplexing greatly depends on
the stability of the oscillation wavelength of a light source. Thus, it is difficult
to perform multiplexing at narrow wavelength (frequency) intervals.
[0006] Therefore, in these years, an optical frequency division multiplexing technique is
known as the all-optical signal multiplexing method. In the optical frequency division
multiplexing technique, signal multiplexing is performed using an all-optical modulator
whose processing speed limit is far beyond the processing speed limit of the electrical
signal. It is unnecessary to separate signals using a multiplexing and demultiplexing
filter, and multiplexed signals can be electrically separated using a single O/E converter
and a typical narrow band RF filter. Thus, the number of O/E converters to be allocated
to multiplexed signals can be greatly reduced, and signals can be highly densely multiplexed
and separated across a wide band.
[0007] In the optical frequency division multiplexing technique, in the case where optical
frequency division multiplexing is performed in all-optical signal multiplexing, an
optical modulator is used in the midway point of a transmission line or in the midway
point of a node. The optical modulator for use in the optical frequency division multiplexing
technique includes a lithium niobate optical modulator (a LNbO
3 modulator) and an electroabsorption modulator, for example. However, these modulators
are devices of a large insertion loss or of large polarization dependence. Moreover,
since the optical modulator modulates electrical signals, the optical modulator has
limitations on the processing speed.
[0008] Therefore, an all-optical modulator is known in which a nonlinear medium is used
and cross phase modulation (XPM) between a carrier light beam and a signal light beam
is used. In a method in which the cross phase modulation effect of a nonlinear medium
is adopted, the processing speed is significantly faster than electrical processing
because processing can be performed at a femto second order response speed due to
the use of the nonlinear optical effect. Moreover, since the method uses an optical
fiber as a nonlinear medium, the method is advantageous in that the insertion loss
is small and coupling to a transmission line is excellent.
[0010] Japanese Laid-open Patent Publication No.
2011-215603.
[0011] However, even the all-optical modulator using a nonlinear medium has polarization
dependence. An ideal polarization state is a state in which the polarization state
of a carrier light beam and the polarization state of a signal light beam are parallel
with each other, and a phase shift amount caused by cross phase modulation becomes
highest. On the other hand, the worst polarization state is a state in which the polarization
state of the carrier light beam and the polarization state of the signal light beam
are orthogonal to each other, and the maximum value of the phase shift amount caused
by cross phase modulation is reduced to one-third, or reduced by 4.8 dB, for example,
from the maximum value as compared with the ideal state. In the case where such an
optical modulator is used to multiplex signals from multiple points, a level difference
of 4.8 dB occurs between multiplexed signals at the maximum. In other words, it can
be said that the all-optical modulator using cross phase modulation greatly depends
on the polarization state of the signal light beam and the polarization state of the
carrier light beam.
[0012] It is also considered to adopt a polarization diversity configuration for a method
of solving polarization dependence. However, although this method can solve polarization
dependence on one hand, the number of parts is increased to hike costs as well as
to increase the insertion loss on the other hand.
[0013] Accordingly, it is an object in one aspect of an embodiment of the invention to provide
an optical frequency division multiplexer and a polarization control method that can
reduce the polarization dependence of an all-optical modulator using cross phase modulation.
SUMMARY
[0014] According to an aspect of an embodiment, an optical frequency division multiplexer
includes a nonlinear medium and a control unit. The nonlinear medium multiplexes,
on a carrier light beam, a signal light beam of a modulation signal that a carrier
signal at a characteristic frequency is modulated with an information signal. The
nonlinear medium cross-phase-modulates the carrier light beam with the signal light
beam, frequency-multiplexes the information signal in the signal light beam on the
carrier light beam. The nonlinear medium generates an optical frequency division multiplexed
signal, and outputs the optical frequency division multiplexed signal. The control
unit controls a polarization state of the signal light beam in a direction in which
an intensity of a modulation component takes a maximum value, based on the intensity
of the modulation component involved in a modulation signal at a desired characteristic
frequency of the optical frequency division multiplexed signal.
BRIEF DESCRIPTION OF DRAWINGS
[0015]
FIG. 1 is an illustration of an exemplary all-optical modulator according to a first
embodiment;
FIGS. 2A and 2B are illustrations in which a polarized pump light wave (a horizontally
linear polarized wave) and a polarized probe light wave (rotated from a horizontally
linear polarized wave to a vertically linear polarized wave) are three-dimensionally
expressed on a Poincare sphere;
FIGS. 3A and 3B are illustrations of an exemplary calculated result of a phase shift
amount by XPM corresponding to the rotation angle of the probe light beam in the example
illustrated in FIGS. 2A and 2B;
FIGS. 4A and 4B are illustrations in which a polarized pump light wave (a right-handed
circularly polarized wave) and a polarized probe light wave (rotated from a horizontally
linear polarized wave to a vertically linear polarized wave) are three-dimensionally
expressed on a Poincare sphere;
FIGS. 5A and 5B are an illustration of an exemplary calculated result of a phase modulation
amount by XPM corresponding to the rotation angle of the probe light beam in the example
illustrated in FIGS. 4A and 4B;
FIGS. 6A and 6B are illustrations in which a polarized pump light wave (a horizontally
linear polarized wave) and a polarized probe light wave (the wave is variable) are
three-dimensionally expressed on a Poincare sphere;
FIG. 7 is an illustration of an exemplary result of actual measurements of the intensity
of a modulation component by XPM corresponding to the rotation angle of the probe
light beam in the example illustrated in FIGS. 6A and 6B;
FIGS. 8A and 8B are illustrations in which a polarized pump light wave (a right-handed
circularly polarized wave) and a polarized probe light wave (the wave is variable)
are three-dimensionally expressed on a Poincare sphere;
FIG. 9 is an illustration of an exemplary result of actual measurements of the intensity
of a modulation component by XPM corresponding to the rotation angle of the probe
light beam in the example illustrated in FIGS. 8A and 8B;
FIG. 10 is an illustration of an exemplary all-optical modulator according to a second
embodiment;
FIG. 11 is an illustration of an exemplary monitoring control unit;
FIG. 12 is an illustration of an exemplary optical network according to a third embodiment;
FIG. 13 is an illustration of an exemplary receiving device;
FIG. 14 is an illustration of an exemplary all-optical modulator according to a fourth
embodiment;
FIG. 15 is an illustration of an exemplary monitoring control unit;
FIG. 16 is an illustration of an exemplary Stokes parameter calculation method used
in a polarization monitor; and
FIG. 17 is an illustration of an exemplary optical network according to a fifth embodiment.
DESCRIPTION OF EMBODIMENTS
[0016] Preferred embodiments of the present invention will be explained with reference to
accompanying drawings.
[0017] It is noted that the disclosed techniques will not be limited by the embodiments.
Moreover, the embodiments described below may be appropriately combined in the scope
with no discrepancy.
[a] First Embodiment
[0018] FIG. 1 is an illustration of an exemplary all-optical modulator according to a first
embodiment. An all-optical modulator 1 illustrated in FIG. 1 is connected to an optical
transmission line 2, and includes a directional coupling unit 11, a nonlinear medium
12, an optical filter 13, an optical branching unit 14, a monitoring control unit
15, an oscillator 16, a mixer 17, a signal light source 18, and a polarization control
unit 19.
[0019] The oscillator 16 can oscillate desired frequencies, and oscillates and outputs a
carrier signal f
i at an RF frequency, for example, which is a characteristic frequency. It is noted
that the characteristic frequency is supposed to be allocated to individual base band
signals B
i, which are information signals. The base band signal B
i is information itself to be transmitted. When the mixer 17 receives the carrier signal
f
i from the oscillator 16 and the base band signal B
i, the mixer 17 modulates the carrier signal f
i with the base band signal B
i to generate a subcarrier modulation signal. Moreover, the mixer 17 outputs the generated
subcarrier modulation signal to the signal light source 18. The signal light source
18 outputs a signal light beam at a center wavelength λs whose subcarrier is modulated.
The polarization control unit 19 controls the polarization state of the signal light
beam λs according to a control signal from the monitoring control unit 15.
[0020] Moreover, the directional coupling unit 11 multiplexes a carrier light beam λc on
the signal light beam λs transmitted from the optical transmission line 2. It is noted
that the carrier light beam λc is a CW (continuous wave) light beam or the like, for
example. The nonlinear medium 12 corresponds to an optical fiber, for example. The
nonlinear medium 12 cross-phase-modulates the carrier light beam λc with the signal
light beam λs, frequency-multiplexes information in the signal light beam λs on the
carrier light beam λc, and generates and outputs an optical frequency division multiplexed
signal.
[0021] The optical filter 13 removes the signal light beam λs outputted from the nonlinear
medium 12, and extracts the carrier light beam λc and the optical frequency division
multiplexed signal. The optical branching unit 14 transmits the extracted carrier
light beam and the extracted optical frequency division multiplexed signal through
the optical transmission line 2, optically branches a part of the light beam and a
part of the signal, and outputs them to the monitoring control unit 15. The monitoring
control unit 15 monitors the intensity of the modulation component of the optical
frequency division multiplexed signal from a part of the carrier light beam and a
part of the optical frequency division multiplexed signal, which are optically branched.
Moreover, the monitoring control unit 15 controls the polarization control unit 19
to control the polarization state of the signal light beam based on the monitored
result.
[0022] Here, the cross phase modulation of the nonlinear medium 12 will be described. Cross
phase modulation is the effect that in the case where a probe light beam such as a
carrier light beam, for example, and a pump light beam such as a signal light beam,
for example, are inputted to the nonlinear medium 12, a refractive index change occurs
in the nonlinear medium 12 corresponding to the intensity of the pump light beam,
and the phase of the probe light beam is modulated.
[0023] Suppose that the intensity of the probe light beam is Ppro, the intensity of the
pump light beam is Ppum, the length of the nonlinear medium 12 is L, the nonlinear
coefficient of the nonlinear medium 12 is γ, and the conditions for the polarization
state of the pump light beam and the polarization state of the probe light beam are
set the same. A nonlinear phase shift amount ϕNL can be expressed by equation ϕNL
= ϕSPM + ϕXPM = γPproL + 2γPpumL.
[0024] The right-hand first term "γPproL" is a nonlinear phase shift amount ϕSPM due to
the light intensity of the probe light beam itself, and caused by self phase modulation
(SPM). Moreover, the right-hand second term "2γPpumL" is a nonlinear phase shift amount
ϕXPM caused by cross phase modulation (XPM) due to the pump light beam, and proportional
to twice a product of the intensity of the pump light beam and the fiber length.
[0025] Furthermore, in the case where the polarization state of the probe light beam and
the polarization state of the pump light beam are in the orthogonal state, the nonlinear
phase shift amount ϕNL can be expressed by equation ϕNL = ϕSPM + ϕXPM = γPproL + 2γPpumL/3.
In other words, since the nonlinear phase shift amount ϕXPM takes 2γPpumL/3, the nonlinear
phase shift amount ϕXPM is reduced to one-third of "2γPpumL" of the maximum value,
that is, reduced by 4.8 dB from the maximum value.
[0026] FIGS. 2A and 2B are illustrations in which a polarized pump light wave (a horizontally
linear polarized wave) and a polarized probe light wave (rotated from a horizontally
linear polarized wave to a vertically linear polarized wave) are three-dimensionally
expressed on a Poincare sphere. FIGS. 3A and 3B are illustrations of an exemplary
calculated result of a phase shift amount by XPM corresponding to the rotation angle
of the probe light beam in the example illustrated in FIGS. 2A and 2B. On the Poincare
sphere illustrated in FIG. 2A, the polarization state of the pump light beam expresses
a horizontally linear polarized wave. On the Poincare sphere illustrated in FIG. 2B,
a vertically linear polarized wave is expressed in which the probe light beam is rotated
at an angle of 90 degrees from a horizontally linear polarized wave along the equator
of the Poincare sphere while the polarization state of the probe light beam is maintaining
the linear polarization state. In the case where the polarization state of the pump
light beam is fixed, for example, the phase shift amount by XPM is changed according
to the rotation operation of the probe light beam. The horizontal axis illustrated
in FIG. 3A expresses a rotation angle θ of the polarization state of the probe light
beam. When the polarization state is two-dimensionally displayed using Jones vectors,
the angle relationship is expressed as illustrated in FIG. 3B. The vertical axis expresses
the calculated result that the phase shift amount by XPM is normalized by a maximum
value. In the case where the rotation angle θ is at an angle of 0 degree and the polarization
state of the pump light beam and the polarization state of the probe light beam are
the same, that is, in the case where the relative angle between the pump light beam
and the probe light beam is at an angle of 0 degree, the phase shift amount by XPM
is the maximum value, "0" dB. Moreover, as illustrated in FIG. 3B, according to the
result of calculating the phase shift amount by XPM corresponding to a change in the
rotation angle θ of the probe light beam, the phase shift amount by XPM is more reduced
as the relative angle between the polarization state of the probe light beam and the
polarization state of the pump light beam becomes greater. In the case where the rotation
angle θ is at an angle of 45 degrees, the phase shift amount by XPM is reduced by
1.8 dB
[0027] from the maximum value. Moreover, in the case where the rotation angle θ is at an
angle of 90 degrees, the phase shift amount by XPM is reduced by 4.8 dB from the maximum
value.
[0028] FIGS. 4A and 4B are illustrations in which a polarized pump light wave (a right-handed
circularly polarized wave) and a polarized probe light wave (rotated from a horizontally
linear polarized wave to a vertically linear polarized wave) are three-dimensionally
expressed on a Poincare sphere. FIGS. 5A and 5B are illustrations of an exemplary
calculated result of a phase shift amount by XPM corresponding to the rotation angle
of the probe light beam in the example illustrated in FIGS. 4A and 4B. On the Poincare
sphere illustrated in FIG. 4A, the polarization state of the pump light beam expresses
a right-handed circularly polarized wave. On the Poincare sphere illustrated in FIG.
4B, a vertically linear polarized wave is expressed in which the probe light beam
is rotated at an angle of 90 degrees from a horizontally linear polarized wave along
the equator of the Poincare sphere while the polarization state of the probe light
beam is maintaining linear polarization. In this state, since the polarization state
of the pump light beam is circular polarization, the relative angle relationship is
maintained as illustrated in FIG. 5B. In FIG. 5A, even though the polarization state
of the probe light beam is rotated from the horizontally linear polarized wave to
the vertically linear polarized wave, the calculated result of a phase shift amount
by XPM takes a constant value by a reduction of 1.8 dB from the maximum value because
the relative angle relationship is consent.
[0029] FIGS. 6A to 9 are diagrams of the result of actual measurements of the intensity
of a modulation component reflecting the phase modulation amount by XPM according
to the rotation operation of the polarization state of the probe light beam. FIGS.
6A and 6B are illustrations in which a polarized pump light wave (a horizontally linear
polarized wave) and a polarized probe light wave (the wave is variable) are three-dimensionally
expressed on a Poincare sphere. FIG. 7 is an illustration of an exemplary result of
actual measurements of the intensity of a modulation component by XPM corresponding
to the rotation angle of the probe light beam in the example illustrated in FIGS.
6A and 6B. On the Poincare sphere illustrated in FIG. 6A, the polarization state of
the pump light beam expresses a horizontally linear polarized wave. On the Poincare
sphere illustrated in FIG. 6B, the case is expressed where the polarization state
of the probe light beam at relative angles with respect to the polarization state
of the pump light beam was rotated from the horizontally linear polarized wave along
the equator of the Poincare sphere. It is noted that seven types of relative angles
were exemplified, an angle of 0 degree, an angle of 15 degrees, an angle of 30 degrees,
an angle of 45 degrees, an angle of 60 degrees, an angle of 75 degrees, and an angle
of 90 degrees, for example, along the equator from the polarization state of the pump
light beam on the equator.
[0030] In FIG. 7, in the case where the relative angle between the polarization state of
the probe light beam and the polarization state of the pump light beam is at an angle
of 0 degree, an angle of 15 degrees, an angle of 30 degrees, or an angle of 45 degrees,
the result of actual measurements was obtained that the intensity of the modulation
component by XPM was reduced by 1.8 dB or less from the maximum value. In contrast
to this, in the case where the relative angle is at an angle of 60 degrees, an angle
of 75 degrees, or an angle of 90 degrees, the result of actual measurements was obtained
that the intensity of the modulation component by XPM was reduced by 4.8 dB at the
maximum beyond 1.8 dB from the maximum value.
[0031] FIGS. 8A and 8B are illustrations in which a polarized pump light wave (a right-handed
circularly polarized wave) and a polarized probe light wave (the wave is variable)
are three-dimensionally expressed on a Poincare sphere. FIG. 9 is an illustration
of an exemplary result of actual measurements of the intensity of a modulation component
by XPM corresponding to the rotation angle of the probe light beam in the example
illustrated in FIGS. 8A and 8B. On the Poincare sphere illustrated in FIG. 8A, the
polarization state of the pump light beam expresses a right-handed circularly polarized
wave. On the Poincare sphere illustrated in FIG. 8B, the case is expressed where the
polarization states of the probe light beams at relative angles were rotated along
parallels of latitude on the Poincare sphere. It is noted that seven types of relative
angles were exemplified, an angle of 0 degree, an angle of 15 degrees, an angle of
30 degrees, an angle of 45 degrees, an angle of 60 degrees, an angle of 75 degrees,
and an angle of 90 degrees, for example, along the longitude line from the polarization
state of the pump light beam on the north pole. In FIG. 9, in the case where the relative
angle between the polarization state of the probe light beam and the polarization
state of the pump light beam is at an angle of 0 degree, an angle of 15 degrees, an
angle of 30 degrees, or an angle of 45 degrees, the result of actual measurements
was obtained that the intensity of the modulation component by XPM was reduced by
about 1.8 dB or less from the maximum value. In contrast to this, in the case where
the relative angle is at an angle of 60 degrees, an angle of 75 degrees, or an angle
of 90 degrees, the result of actual measurements was obtained that the intensity of
the modulation component by XPM was reduced by 4.8 dB at the maximum beyond 1.8 dB
from the maximum value.
[0032] As a result, in the case where the relative angle between the polarization state
of the probe light beam and the polarization state of the pump light beam is within
an angle of 45 degrees, in other words, in the case where the polarization state of
the probe light beam and the polarization state of the pump light beam are on the
same hemisphere of the Poincare sphere, it is revealed that a reduction in the intensity
of the modulation component by XPM can be suppressed within 1.8 dB.
[0033] Therefore, based on such results, the foregoing all-optical modulator 1 according
to the first embodiment will be described. The foregoing probe light beam corresponds
to the carrier light beam, for example, and the pump light beam corresponds to the
signal light beam, for example. Since the carrier light beam propagates through the
optical transmission line 2 such as an optical fiber, the polarization state fluctuates
due to the vibrations of the optical transmission line 2, for example, and an environmental
change such as the temperature, for example. Since the all-optical modulator 1 receives
the carrier light beam in the state in which the polarization state fluctuates, the
intensity of the modulation component of the nonlinear medium 12 subjected to optical
frequency division multiplexing by XPM is reduced by 4.8 dB at the maximum.
[0034] Therefore, the monitoring control unit 15 in the all-optical modulator 1 monitors
the intensity of the modulation component of the optical frequency division multiplexed
signal. Moreover, in the case where the intensity of the modulation component is reduced
beyond 1.8 dB from the maximum value, the monitoring control unit 15 controls the
polarization control unit 19 to control the polarization state of the signal light
beam in such a way that the maximum value of the intensity of the modulation component
is not reduced beyond 1.8 dB. It is noted that the case where the maximum value of
the intensity of the modulation component is reduced beyond 1.8 dB means that the
polarization state of the signal light beam exists on a hemisphere different from
a hemisphere on which the polarization state of the carrier light beam exists when
the polarization states are expressed on the Poincare sphere. The polarization control
unit 19 converts the polarization state of the signal light beam at an angle of 90
degrees in such a way that the polarization state of the signal light beam is positioned
on the same hemisphere on which the polarization state of the carrier light beam exists.
The polarization control unit 19 then inputs the signal light beam whose the polarization
state is converted at an angle of 90 degrees to the directional coupling unit 11.
[0035] As a result, since the polarization state of the signal light beam and the polarization
state of the carrier light beam are positioned on the same hemisphere, that is, since
the relative angle between the signal light beam and the carrier light beam is within
an angle of 45 degrees, a reduction in the intensity of the modulation component of
the optical frequency division multiplexed signal by XPM in the nonlinear medium 12
can be suppressed within 1.8 dB. Moreover, since a single optical branching unit 14
is provided to branch the optical frequency division multiplexed signal, the monitoring
control unit 15 can also suppress the insertion loss caused by the optical branching
unit 14.
[0036] The all-optical modulator 1 according to the first embodiment monitors the intensity
of the modulation component of the optical frequency division multiplexed signal,
and converts the polarization state of the signal light beam at an angle of 90 degrees,
in the case where the intensity is reduced beyond 1.8 dB from the maximum value. As
a result, a reduction in the intensity of the modulation component caused by the polarization
dependence of XPM can be decreased.
[0037] Moreover, the all-optical modulator 1 monitors the polarization state of the signal
light beam and the polarization state of the carrier light beam, and rotates the polarization
state of the signal light beam at an angle of 90 degrees in such a way that the polarization
state of the signal light beam is positioned on the same hemisphere on which the polarization
state of the carrier light beam exists, in the case where the polarization state of
the signal light beam exists on a hemisphere different from a hemisphere on which
the polarization state of the carrier light beam exists. As a result, a reduction
in the intensity of the modulation component of the optical frequency division multiplexed
signal caused by the polarization dependence of XPM can be decreased.
[0038] It is noted that the monitoring control unit 15 of the all-optical modulator 1 according
to the first embodiment converts the polarization state of the signal light beam at
an angle of 90 degrees, in the case where the intensity of the modulation component
of the optical frequency division multiplexed signal is reduced beyond 1.8 dB from
the maximum value. However, the threshold at which the polarized light is rotated
is not limited to a point in time at which the intensity exceeds 1.8 dB from the maximum
value. Such a configuration may be possible in which the threshold is set to a given
point in time in the range in which the intensity is reduced by 4.8 dB beyond 1.8
dB from the maximum value and the polarization state of the signal light beam is converted
at an angle of 90 degrees.
[b] Second Embodiment
[0039] FIG. 10 is an illustration of an exemplary all-optical modulator according to a second
embodiment. It is noted that the same reference numerals and signs are designated
to the same configurations of the all-optical modulator 1 illustrated in FIG. 1, and
the description of the overlapping configurations and operations is omitted. An all-optical
modulator 1A illustrated in FIG. 10 includes an optical coupler 11A, a nonlinear medium
12A, an optical filter 13A, an optical coupler 14A, a monitoring control unit 15A,
an oscillator 16A, a mixer 17A, a signal light source 18A, and a polarization control
unit 19A.
[0040] The oscillator 16A oscillates and outputs a carrier signal f
i at an RF frequency, for example, which is a characteristic frequency. When the mixer
17A receives a carrier signal f
i from the oscillator 16A and a base band signal B
i, the mixer 17A modulates the carrier signal f
i with the base band signal B
i to generate a subcarrier modulation signal. Moreover, the mixer 17A outputs the generated
subcarrier modulation signal to the signal light source 18A. The signal light source
18A outputs a signal light beam at a center wavelength λs whose subcarrier is modulated.
The polarization control unit 19A controls the polarization state of the signal light
beam λs according to a control signal from the monitoring control unit 15A.
[0041] Furthermore, the optical coupler 11A multiplexes a carrier light beam λc on the signal
light beam λs transmitted from the optical transmission line 2. The nonlinear medium
12A corresponds to a high nonlinear fiber, for example. The nonlinear medium 12A cross-phase-modulates
the carrier light beam λc with the signal light beam λs, frequency-multiplexes information
in the signal light beam λs on the carrier light beam λc, and generates and outputs
an optical frequency division multiplexed signal.
[0042] The optical filter 13A extracts the carrier light beam λc and the optical frequency
division multiplexed signal outputted from the nonlinear medium 12A. The optical coupler
14A transmits the extracted carrier light beam and the extracted optical frequency
division multiplexed signal through the optical transmission line 2, optically branches
a part of the light beam and a part of the signal, and outputs them to the monitoring
control unit 15A. The monitoring control unit 15A monitors the intensity of the modulation
component of the optical frequency division multiplexed signal from a part of the
carrier light beam and a part of the optical frequency division multiplexed signal,
which are optically branched. Moreover, the monitoring control unit 15A controls the
polarization control unit 19A to control the polarization state of the signal light
beam based on the monitored result.
[0043] FIG. 11 is an illustration of an exemplary monitoring control unit 15A. The monitoring
control unit 15A illustrated in FIG. 11 includes a phase intensity converter circuit
21, a photodetector 22, an RF filter 23, a detector 24, an A/D converter circuit 25,
a memory 26, an arithmetic operation circuit 27, and a driver circuit 28. It is noted
that since the optical frequency division multiplexed signal is a cross phase modulation
signal, the modulation component appears on the upper wave band and the lower wave
band of the carrier light beam. The phases of the modulation components are inverted
to each other at an angle of 90 degrees on the upper wave band and on the lower wave
band. Therefore, even though the photodetector 22 receives the carrier light beam,
the phases are canceled with each other when the phases are detected simultaneously,
and the intensity of the modulation component is not enabled to be detected. Thus,
the monitoring control unit 15A contains the phase intensity converter circuit 21
that converts the phase modulation signal of the optical frequency division multiplexed
signal into an intensity modulated signal. For the phase intensity converter circuit
21, the following may be used such as a dispersive medium (a dispersion-compensating
fiber) corresponding to a frequency band, a coherent receiver including a local light
beam (LO), and an optical filter that removes a modulation component of one of the
upper wave band and the lower wave band.
[0044] The phase intensity converter circuit 21 converts the phase modulation signal of
a part of the optical frequency division multiplexed signal optically branched at
the optical coupler 14A into an intensity modulated signal. The photodetector 22 optoelectrically
converts the intensity modulated signal that is an optical signal. The RF filter 23
extracts a modulation component at a desired characteristic frequency from the optoelectrically
converted intensity modulated signal. The detector 24 detects the extracted modulation
component at a desired characteristic frequency, and outputs a voltage signal. The
A/D converter circuit 25 digitally converts the voltage signal of the modulation component,
and stores the signal in the memory 26 as the intensity of the modulation component.
[0045] The arithmetic operation circuit 27 compares the history of the intensity of the
modulation component stored in the memory 26, determines whether the intensity of
the modulation component at a characteristic frequency is reduced beyond a predetermined
threshold from the maximum value, and outputs the determined result to the driver
circuit 28. It is noted that the arithmetic operation circuit 27 determines whether
the intensity of the modulation component is reduced beyond a predetermined threshold
of 1.8 dB, for example. In the case where the intensity of the modulation component
is reduced beyond 1.8 dB, the driver circuit 28 outputs a control signal to instruct
the polarization control unit 19A to rotate the polarization state of the signal light
beam at an angle of 90 degrees. The polarization control unit 19A controls the polarization
state of the signal light beam in response to the control signal from the driver circuit
28.
[0046] As a result, in the case where the intensity of the modulation component is reduced
beyond 1.8 dB from the maximum value, the polarization state of the signal light beam
is rotated at an angle of 90 degrees, so that a reduction in the intensity of the
modulation component can be suppressed within 1.8 dB from the maximum value.
[0047] It is noted that for the polarization control unit 19A, the following may be used
such as a device equipped with a wave plate, a fiber squeezer device (a fiber stress
applying device), a liquid crystal device, and a faraday rotator device, for example.
For example, a polarization switch (a product name of Pola Switch) commercially available
from General Photonics Corporation can rotate the polarization state of the signal
light beam at an angle of 90 degrees by applying a voltage of 2 to 3 V.
[0048] The all-optical modulator 1A according to the second embodiment monitors the intensity
of the modulation component of the optical frequency division multiplexed signal,
and converts the polarization state of the signal light beam at an angle of 90 degrees,
in the case where the intensity of the modulation component is reduced beyond 1.8
dB from the maximum value. As a result, a reduction in the intensity of the modulation
component of the optical frequency division multiplexed signal caused by the polarization
dependence of XPM can be decreased.
[0049] Moreover, since the all-optical modulator 1A includes a single optical branching
unit 14 that branches the optical frequency division multiplexed signal as compared
with a polarization diversity configuration, the insertion loss caused by the optical
branching unit 14 can be suppressed.
[0050] It is noted that the monitoring control unit 15A of the all-optical modulator 1A
according to the second embodiment converts the polarization state of the signal light
beam at an angle of 90 degrees, in the case where the intensity of the modulation
component is reduced beyond 1.8 dB from the maximum value. However, the threshold
at which the polarized light is rotated is not limited to a point in time at which
the intensity exceeds 1.8 dB from the maximum value. Such a configuration may be possible
in which the threshold is set to a given point in time in the range in which the intensity
is reduced by 4.8 dB beyond 1.8 dB from the maximum value and the polarization state
of the signal light beam is converted at an angle of 90 degrees.
[0051] In the second embodiment, the monitoring control unit 15A is contained in the all-optical
modulator 1A. However, the monitoring control unit may be contained in a receiving
device that receives the optical frequency division multiplexed signal, not contained
in the all-optical modulator 1A. In the following, an embodiment in this case will
be described as a third embodiment.
[c] Third Embodiment
[0052] FIG. 12 is an illustration of an exemplary optical network according to a third embodiment.
An optical network 30 illustrated in FIG. 12 includes a carrier light source 31, a
plurality of all-optical modulators 1B-1 to 1B-n, and a receiving device 3. The all-optical
modulator 1B-1 is connected to the all-optical modulator 1B-j with an optical transmission
line 2-1. Moreover, the all-optical modulator 1B-j is connected to the all-optical
modulator 1B-n with an optical transmission line 2-j. Furthermore, the all-optical
modulator 1B-n is connected to the receiving device 3 with an optical transmission
line 2-n.
[0053] The all-optical modulator 1B-j includes an optical coupler 11B, a nonlinear medium
12B, an optical filter 13B, an oscillator 16B, a mixer 17B, a signal light source
18B, and a polarization control unit 19B.
[0054] The oscillator 16B oscillates and outputs a carrier signal f
i at an RF frequency, for example, which is a characteristic frequency. When the mixer
17B receives a carrier signal f
i from the oscillator 16B and a base band signal B
i, the mixer 17B modulates the carrier signal f
i with the base band signal B
i to generate a subcarrier modulation signal. Moreover, the mixer 17B outputs the generated
subcarrier modulation signal to the signal light source 18B. The signal light source
18B outputs a signal light beam at a center wavelength λs whose subcarrier is modulated.
The polarization control unit 19B controls the polarization state of the signal light
beam λs according to a control signal from the receiving device 3.
[0055] Furthermore, the optical coupler 11B multiplexes a carrier light beam λc on the signal
light beam λs transmitted from the optical transmission line 2. The nonlinear medium
12B corresponds to a high nonlinear fiber, for example. The nonlinear medium 12B cross-phase-modulates
the carrier light beam λc with the signal light beam λs, frequency-multiplexes information
in the signal light beam λs on the carrier light beam λc, and generates and outputs
an optical frequency division multiplexed signal. The optical filter 13B extracts
the carrier light beam λc and the optical frequency division multiplexed signal outputted
from the nonlinear medium 12B, and outputs the extracted carrier light beam λc and
the extracted optical frequency division multiplexed signal to the optical transmission
line 2-j. It is noted that since the internal configurations of the other all-optical
modulators 1B-1 and 1B-n are the same as the internal configuration of the all-optical
modulator 1B-j, the same reference numerals and signs are designated to the same configurations,
and the description of the overlapping configurations and operations is omitted.
[0056] The all-optical modulator 1B-1 cross-phase-modulates the carrier light beam from
the carrier light source 31 with the signal light beam, and transmits the optical
frequency division multiplexed signal to the optical transmission line 2-1. The all-optical
modulator 1B-j receives the optical frequency division multiplexed signal from an
optical transmission line 2-j-1, cross-phase-modulates the carrier light beam of the
optical frequency division multiplexed signal with the signal light beam, and transmits
the optical frequency division multiplexed signal to the optical transmission line
2-j. Moreover, the all-optical modulator 1B-n receives the optical frequency division
multiplexed signal from an optical transmission line 2-n-1, cross-phase-modulates
the carrier light beam of the optical frequency division multiplexed signal with the
signal light beam, and transmits the optical frequency division multiplexed signal
to the optical transmission line 2-n.
[0057] Furthermore, the receiving device 3 receives the optical frequency division multiplexed
signal from the optical transmission line 2-n. The receiving device 3 includes a receiver
40 and a monitoring control unit 50. FIG. 13 is an illustration of an exemplary receiving
device 3. The receiver 40 illustrated in FIG. 13 includes a phase intensity converter
circuit 41, a photodetector 42, a power divider 43, a plurality of RF filters 44,
a plurality of power dividers 45, and a demodulator circuit 46. It is noted that the
RF filters 44 and the power dividers 45 are individually provided for the characteristic
frequencies of carrier signals multiplexed in the optical frequency division multiplexed
signal.
[0058] The phase intensity converter circuit 41 converts the phase modulation signal of
the optical frequency division multiplexed signal into an intensity modulated signal.
The photodetector 42 optoelectrically converts the intensity modulated signal that
is an optical signal. The power divider 43 that branches the optical frequency division
multiplexed signal for the channels of the characteristic frequencies of modulation
components multiplexed in the optical frequency division multiplexed signal, and outputs
the signals to the RF filters 44. It is noted that the power divider 43 may use amplifiers
corresponding to the number of branches because the power divider 43 branches the
optical frequency division multiplexed signal for the channels of characteristic frequencies.
[0059] The RF filters 44 individually extract a modulation component at a desired characteristic
frequency multiplexed in the optical frequency division multiplexed signal. The power
dividers 45 branch the extracted modulation component at the characteristic frequency,
and output the modulation component to the demodulator circuits 46 and the monitoring
control unit 50. The demodulator circuits 46 demodulate the modulation component at
the characteristic frequency into an information signal, and output data. It is noted
that for the demodulator circuit 46, the following may be used such as an envelope
detector, a square-law detector, a synchronous detector, a phase detector, and a frequency
detector, for example.
[0060] The monitoring control unit 50 includes a plurality of detectors 51, a plurality
of A/D converter circuits 52, a plurality of memories 53, an arithmetic operation
circuit 54, and a plurality of driver circuits 55. The detectors 51, the A/D converter
circuits 52, the memories 53 and the driver circuits 55 are individually provided
for the characteristic frequencies of carrier signals multiplexed in the optical frequency
division multiplexed signal. It is noted that a single arithmetic operation circuit
54 is provided. However, the arithmetic operation circuit 54 may be individually provided
for characteristic frequencies.
[0061] The detectors 51 detect a modulation component at a desired characteristic frequency
divided at the power dividers 45 in the receiver 40, and output a voltage signal.
The A/D converter circuits 52 digitally convert the voltage signal of the modulation
component, and stores the voltage signal as the intensity of the modulation component
in the memories 53.
[0062] The arithmetic operation circuit 54 compares the history of the intensity of the
modulation component stored in the memories 53, determines whether the intensity of
the modulation component at a characteristic frequency is reduced beyond a predetermined
threshold from the maximum value for the individual modulation components at characteristic
frequencies, and outputs the determined results of the individual modulation components
at the characteristic frequencies to the driver circuits 55. It is noted that the
arithmetic operation circuit 54 determines whether the intensity of the modulation
component is reduced beyond a predetermined threshold of 1.8 dB, for example.
[0063] In the case where the intensity of the modulation component at a characteristic frequency
is reduced beyond a predetermined threshold, the driver circuit 55 outputs, to the
polarization control unit 19B, a control signal to control the polarization state
of the signal light beam that the carrier signal at the characteristic frequency is
modulated according to the determined result of the modulation component at the characteristic
frequency. The polarization control unit 19B in the all-optical modulator 1B converts
the polarization state of the signal light beam at an angle of 90 degrees in response
to the control signal.
[0064] As a result, the monitoring control unit 50 in the receiving device 3 monitors the
intensities of the modulation components at the characteristic frequencies subjected
to cross phase modulation at the all-optical modulators 1B-1 to 1B-n. In the case
where the intensity of the modulation component at a characteristic frequency is reduced
beyond 1.8 dB from the maximum value, the monitoring control unit 50 outputs a control
signal to the polarization control unit 19B that controls the polarization state of
the signal light beam in such a way that the polarization state of the signal light
beam involved in the modulation component at the characteristic frequency is converted
at an angle of 90 degrees. Namely, the monitoring control unit 50 in the receiving
device 3 collectively monitors the intensities of the modulation components at characteristic
frequencies in the optical frequency division multiplexed signals modulated at the
all-optical modulators 1B-1 to 1B-n in the optical network 30, and controls the polarization
control unit 19B on the individual all-optical modulators based on the monitored results.
[0065] The monitoring control unit 50 in the receiving device 3 according to the third embodiment
monitors the intensities of the modulation components at characteristic frequencies
subjected to cross phase modulation at the all-optical modulators 1B-1 to 1n. In the
case where the intensity of the modulation component at a characteristic frequency
is reduced beyond 1.8 dB from the maximum value, the monitoring control unit 50 outputs
a control signal to the polarization control unit 19B that controls the polarization
state of the signal light beam in such a way that the polarization state of the signal
light beam involved in the modulation component at the characteristic frequency is
converted at an angle of 90 degrees. As a result, it is unnecessary for the all-optical
modulators to contain the monitoring control unit and to include the optical coupler
to branch a part of the optical frequency division multiplexed signal, so that the
number of parts of the overall optical network 30 can be greatly reduced as well as
the optical insertion loss of the optical frequency division multiplexed signal can
be reduced. Moreover, a reduction in the intensity of the modulation component caused
by the polarization dependence of XPM can be suppressed.
[0066] It is noted that the monitoring control unit 50 in the receiving device 3 converts
the polarization state of the signal light beam at an angle of 90 degrees, in the
case where the intensity of the modulation component of the optical frequency division
multiplexed signal is reduced beyond 1.8 dB from the maximum value. However, the threshold
at which the polarized light is rotated is not limited to a point in time at which
the intensity exceeds 1.8 dB from the maximum value. Such a configuration may be possible
in which the threshold is set to a given point in time in the range in which the intensity
is reduced by 4.8 dB beyond 1.8 dB from the maximum value and the polarization state
of the signal light beam is converted at an angle of 90 degrees.
[0067] Moreover, the monitoring control unit 15A of the all-optical modulator 1A according
to the second embodiment cross-phase-modulates the carrier light beam with the signal
light beam at the nonlinear medium 12A, optically branches a part of the optical frequency
division multiplexed signal to monitor the modulation component at a characteristic
frequency, and controls the polarization state of the signal light beam based on the
monitored result. However, such a configuration may be possible in which a polarization
monitor that monitors the polarization state of the carrier light beam and the polarization
state of the signal light beam is used prior to the cross phase modulation of the
carrier light beam and the signal light beam at the nonlinear medium 12A. In the following,
an embodiment in this case will be described as a fourth embodiment.
[d] Fourth Embodiment
[0068] FIG. 14 is an illustration of an exemplary all-optical modulator 1C according to
a fourth embodiment. The all-optical modulator 1C illustrated in FIG. 14 includes
an optical coupler 11C, a nonlinear medium 12C, an optical filter 13C, a monitoring
control unit 15C, an oscillator 16C, a mixer 17C, a signal light source 18C, and a
polarization control unit 19C.
[0069] The oscillator 16C oscillates and outputs a carrier signal f
i at an RF frequency, for example, which is a characteristic frequency. When the mixer
17C receives a carrier signal f
i from the oscillator 16C and a base band signal B
i, the mixer 17C modulates the carrier signal f
i with the base band signal B
i to generate a subcarrier modulation signal. Moreover, the mixer 17C outputs the generated
subcarrier modulation signal to the signal light source 18C. The signal light source
18C outputs a signal light beam at a center wavelength λs whose subcarrier is modulated.
The polarization control unit 19C controls the polarization state of the signal light
beam λs according to a control signal from the monitoring control unit 15C.
[0070] Moreover, the optical coupler 11C multiplexes a carrier light beam λc on the signal
light beam λs transmitted from the optical transmission line 2. The nonlinear medium
12C corresponds to a high nonlinear fiber, for example. The nonlinear medium 12C cross-phase-modulates
the carrier light beam λc with the signal light beam λs, frequency-multiplexes information
in the signal light beam λs on the carrier light beam λc, and generates and outputs
an optical frequency division multiplexed signal.
[0071] The optical filter 13C extracts the carrier light beam λc and the optical frequency
division multiplexed signal outputted from the nonlinear medium 12C. The monitoring
control unit 15C optically branches a part of the carrier light beam and a part of
the signal light beam at the optical coupler 11C, and monitors the polarization state
of the carrier light beam and the polarization state of the signal light beam, which
are optically branched. It is noted that it is unnecessary to use a two-input-two-output
optical coupler for the optical coupler 11C. Such a configuration may be possible
in which a carrier light beam and a signal light beam are multiplexed with each other
at a low transmission loss using a WDM coupler or the like and then a part of power
is branched using a power branching optical coupler. Moreover, the monitoring control
unit 15C controls the polarization control unit 19C to control the polarization state
of the signal light beam based on the monitored result.
[0072] FIG. 15 is an illustration of an exemplary monitoring control unit 15C. The monitoring
control unit 15C illustrated in FIG. 15 includes an optical filter 61, a polarization
monitor 62, a memory 63, an arithmetic operation circuit 64, and a driver circuit
65. The optical filter 61 extracts a carrier light beam or a signal light beam. The
polarization monitor 62 corresponds to a polarimeter, for example, and monitors the
polarization state of the extracted carrier light beam or the extracted signal light
beam. The polarization monitor 62 temporarily blocks the input of the carrier light
beam, and records the polarization state of the signal light beam in the state in
which the transmission band of the optical filter 61 is matched with the signal light
beam λs, in order to monitor the polarization state of the carrier light beam or the
polarization state of the signal light beam using a single polarimeter. In the blocking
and recording, since the signal light beam does not propagate through the transmission
line, the polarization state can be maintained at constant by a configuration in which
the lengths of fibers between a polarization controller, an optical coupler, and a
monitoring control circuit coupler, through which the signal light beam propagates,
are shortened as short as possible, or using a polarization maintaining fiber. After
that, the polarization monitor 62 monitors the polarization state of the carrier light
beam by matching the transmission band of the optical filter 61 with the carrier wavelength
λc, and grasps the relative angle between the polarization state of the signal light
beam and the polarization state of the carrier light beam on the same Poincare sphere
surface.
[0073] Moreover, the polarization monitor 62 sections hemispheres at the equator or the
longitude line depending on a hemisphere at which position the hemisphere is on the
Poincare sphere surface, the hemisphere including a polarization plane rotated at
an angle of 90 degrees with respect to the polarization state of the signal light
beam. For example, in the case where the polarization state of the signal light beam
is a right-handed circularly polarized wave, the polarization monitor 62 sections
hemispheres at the equator (see FIGS. 8A and 8B). Furthermore, for example, in the
case where the polarization state of the signal light beam is a horizontally linear
polarized wave, the polarization monitor 62 sections hemispheres at the longitude
line of the polarization state of the signal light beam (see FIGS. 6A and 6B).
[0074] In addition, the polarization monitor 62 observes the polarization state of the carrier
light beam using Stokes parameters, for example, and stores the observed result in
the memory 63. FIG. 16 is an illustration of an exemplary measurement circuit in the
polarization monitor 62. A measurement circuit 200 illustrated in FIG. 16 is a circuit
that measures Stokes parameters. The measurement circuit 200 includes a first optical
coupler 201, a second optical coupler 202, a third optical coupler 203, a first PD
204, a second PD 205, a third PD 206, and a fourth PD 207. The measurement circuit
200 further includes a first polarizer 208, a second polarizer 209, a third polarizer
210, and a quarter-wave plate 211.
[0075] The first optical coupler 201 optically branches the optical signal at a ratio of
three to one, and inputs 25% of the total optical signal to the second PD 205 side.
The second optical coupler 202 optically branches the optical signal from the first
optical coupler 201 at a ratio of two to one, and inputs 25% of the total optical
signal to the third PD 206 side. The third optical coupler 203 optically branches
the optical signal from the second optical coupler 202 at a ratio of one to one, and
inputs 25% of the total optical signal to the fourth PD 207 side and the first PD
204.
[0076] Furthermore, the second PD 205 receives, from the first optical coupler 201, the
optical signal transmitted through the first polarizer 208 whose reference plane is
at an angle of 0°, and obtains a light intensity PD2. The third PD 206 receives, from
the second optical coupler 202, the optical signal transmitted through the second
polarizer 209 tilted at an angle of 45° with respect to the reference plane, and obtains
a light intensity PD3. The fourth PD 207 receives, from the third optical coupler
203, the optical signal transmitted through the quarter-wave plate 211 and the third
polarizer 210 tilted at an angle of 45° with respect to the reference plane, and obtains
a light intensity PD4. In addition, the first PD 204 receives the optical signal from
the third optical coupler 203, and obtains a light intensity PD1.
[0077] Stokes parameters S
0, S
1, S
2 and S
3 can be expressed by equations S
0 = PD1, S
1 = 2PD2 - PD1, S
2 = 2PD3 - PD1, and S
3 = 2PD4 - PD1, for example, using the light intensities P1, P2, P3 and P4. S
0 expresses the intensity of inputted light, S
1 expresses a horizontally linear polarized component (at an angle of 0 degree), S
2 expresses a linear polarized component tilted at an angle of 45 degrees, and S
3 expresses a right-handed circularly polarized component. Completely polarized light
can be expressed by equation S
02 = S
12 + S
22 + S
32.
[0078] A sphere can be generated as a Poincare sphere. The sphere is positioned at one point
on a spherical surface in which the Stokes parameters S
1, S
2 and S
3 of the Stokes parameters (S
0, S
1, S
2, and S
3) are set to the axes of a space rectangular coordinate system and the intensity S
0 is a radius.
[0079] Subsequently, the arithmetic operation circuit 64 calculates a relative angle between
the polarization state of the signal light beam and the polarization state of the
carrier light beam acquired at the polarization monitor, and determines whether the
polarization state of the carrier light beam is on a hemisphere different from a hemisphere
on which the polarization state of the signal light beam exists based on the calculated
relative angle.
[0080] For example, in the case where the polarization state of the signal light beam is
a right-handed circularly polarized wave, the arithmetic operation circuit 64 sections
hemispheres at the equator as illustrated in FIGS. 8A and 8B, and determines whether
the polarization state of the carrier light beam is on a hemisphere different from
a hemisphere on which the polarization state of the signal light beam exists. In the
case where the polarization state of the carrier light beam is on a hemisphere different
from a hemisphere on which the polarization state of the signal light beam exists,
the driver circuit 65 outputs a control signal to the polarization control unit 19C
to rotate the polarization state of the signal light beam whose relative angle is
at an angle of 60 degrees, an angle of 75 degrees, or an angle of 90 degrees, for
example, at an angle of 90 degrees. The polarization control unit 19C moves the polarization
state of the carrier light beam whose relative angle is at an angle of 60 degrees,
an angle of 70 degrees, or an angle of 90 degrees, for example, on the same hemisphere
on which the polarization state of the signal light beam exists according to the conversion
at an angle of 90 degrees. As a result, the relative angle between the polarization
state of the carrier light beam and the polarization state of the signal light beam
is within an angle of 45 degrees, so that a reduction in the intensity of the modulation
component caused by the polarization dependence of XPM can be greatly reduced.
[0081] Moreover, for example, in the case where the polarization state of the signal light
beam is a horizontally linear polarized wave, the arithmetic operation circuit 64
sections hemispheres at the longitude line at which the polarization state of the
signal light beam is positioned as illustrated in FIGS. 6A and 6B, and determines
whether the polarization state of the carrier light beam is on a hemisphere different
from a hemisphere on which the polarization state of the signal light beam exists.
In the case where the polarization state of the carrier light beam is on a hemisphere
different from a hemisphere on which the polarization state of the signal light beam
exists, the driver circuit 65 outputs a control signal to the polarization control
unit 19C to rotate the polarization state of the signal light beam whose relative
angle is at an angle of 60 degrees, an angle of 75 degrees, or an angle of 90 degrees,
for example, at an angle of 90 degrees. The polarization control unit 19C moves the
polarization state of the carrier light beam whose relative angle is at an angle of
60 degrees, an angle of 70 degrees, or an angle of 90 degrees, for example, on the
same hemisphere on which the polarization state of the signal light beam exists according
to the conversion at an angle of 90 degrees. As a result, the relative angle between
the polarization state of the carrier light beam and the polarization state of the
signal light beam is within an angle of 45 degrees, so that a reduction in the intensity
of the modulation component caused by the polarization dependence of XPM can be greatly
reduced.
[0082] It is noted that for the polarization control unit 19C, the following may be used
such as a device equipped with a wave plate, a fiber squeezer device (a fiber stress
applying device), a liquid crystal device, and a faraday rotator device, for example.
For example, a polarization switch (a product name of Pola Switch) commercially available
from General Photonics Corporation can rotate the polarization state of the signal
light beam at an angle of 90 degrees by applying a voltage of 2 to 3 V.
[0083] The all-optical modulator 1C according to the fourth embodiment monitors the polarization
state of the carrier light beam and the polarization state of the signal light beam
and controls the polarization state of the carrier light beam and the polarization
state of the signal light beam in the same hemisphere all the time, so that a reduction
in the intensity of the modulation component caused by the polarization dependence
of XPM in the nonlinear medium 12C can be reduced.
[0084] Moreover, the all-optical modulator 1C has only an insertion loss caused by the optical
coupler 11C added to the carrier light beam side as compared with a polarization diversity
configuration, so that the insertion loss can be reduced.
[0085] It is noted that in the first to fourth embodiments, in the case where the polarization
state of the carrier light beam fluctuates on the optical transmission line 2, the
polarization state of the signal light beam is controlled. In the following, an embodiment
in the case where the polarization state of the signal light beam fluctuates will
be described as a fifth embodiment.
[e] Fifth Embodiment
[0086] FIG. 17 is an illustration of an exemplary optical network according to a fifth embodiment.
An optical network 30A illustrated in FIG. 17 includes a plurality of transmitting
devices 70
1 to 70
n, a plurality of optical transmission lines 74
1 to 74
n, and an optical transmitting device 80. The transmitting devices 70
1 to 70
n include an oscillator 71, a mixer 72, and a signal light source 73.
[0087] The oscillator 71 oscillates and outputs a carrier signal f at an RF frequency, for
example, which is a characteristic frequency. When the mixer 72 receives the carrier
signal f from the oscillator 71 and a base band signal B, the mixer 72 modulates the
carrier signal f with the base band signal B to generate a subcarrier modulation signal.
Moreover, the mixer 72 outputs the generated subcarrier modulation signal to the signal
light source 73. The signal light source 73 outputs a signal light beam whose subcarrier
is modulated.
[0088] The optical transmitting device 80 is connected to optical transmission lines 74
1 to 74
n that are individually connected to transmitting devices 70
1 to 70
n, and receives individual signal light beams from the transmitting devices 70
1 to 70
n through the optical transmission lines 74
1 to 74
n. The optical transmitting device 80 includes a carrier light source 81, a plurality
of all-optical modulation units 90
1 to 90
n, a plurality of polarization control units 82
1 to 82
n, and a receiving unit 100. The all-optical modulation units 90
1 to 90
n and the polarization control units 82
1 to 82
n are individually disposed on the optical transmission lines 74
1 to 74
n involved in the transmitting devices 70
1 to 70
n.
[0089] The carrier light source 81 outputs a carrier light beam at a wavelength λc. The
all-optical modulation units 90
1 to 90
n include an optical coupler 91, a nonlinear medium 92, and an optical filter 93. The
optical coupler 91 multiplexes the carrier light beam λc transmitted from the carrier
light source 81 with a signal light beam. The nonlinear medium 92 corresponds to a
high nonlinear fiber, for example. The nonlinear medium 92 cross-phase-modulates the
carrier light beam λc with the signal light beam, frequency-multiplexes information
in the signal light beam on the carrier light beam λc, and generates and outputs an
optical frequency division multiplexed signal. The optical filter 93 extracts the
carrier light beam λc and the optical frequency division multiplexed signal outputted
from the nonlinear medium 92.
[0090] The all-optical modulation units 90
1 to 90
n cross-phase-modulate the carrier light beam with the signal light beams, and output
the carrier light beam λc and an optical frequency division multiplexed signal. The
all-optical modulation unit 90n then outputs the optical frequency division multiplexed
signal to the receiving unit 100. The receiving unit 100 includes a phase intensity
converter circuit 101, a photodetector 102, a power divider 103, a plurality of RF
filters 104, and a monitoring control unit 105.
[0091] The phase intensity converter circuit 101 converts the phase modulation signal of
the optical frequency division multiplexed signal from the all-optical modulation
unit 90
n into an intensity modulated signal. The photodetector 102 optoelectrically converts
the intensity modulated signal that is an optical signal. The power divider 103 branches
the intensity modulated signal by the number of the transmitting devices 70, and outputs
the branched intensity modulated signals to the RF filters 104. The RF filters 104
extract a modulation component at a desired characteristic frequency from the optoelectrically
converted intensity modulated signal. The RF filters 104 output data of the extracted
modulation component at a characteristic frequency, and output a part of the data
to the monitoring control unit 105.
[0092] The monitoring control unit 105 detects the extracted modulation component at a desired
characteristic frequency for the individual RF filters 104, and detects the intensity
of the modulation component. Moreover, the monitoring control unit 105 determines
whether the intensity of the modulation component at a characteristic frequency is
reduced beyond a predetermined threshold of 1.8 dB, for example, from the maximum
value. In the case where the intensity of the modulation component is reduced beyond
1.8 dB, the monitoring control unit 105 outputs, to the polarization control units
82
1 to 82
n, a control signal to instruct the polarization state of the signal light beam at
a relevant characteristic frequency to be rotated at an angle of 90 degrees.
[0093] The polarization control units 82
1 to 82
n control the polarization state of the signal light beam propagating through the optical
transmission lines 74
1 to 74
n for the individual transmitting devices 70
1 to 70
n in response to the control signal. In the case where the intensity of the modulation
component is reduced beyond 1.8 dB from the maximum value, the polarization state
of the signal light beam is rotated at an angle of 90 degrees. As a result, a reduction
in the intensity of the modulation component can be suppressed within 1.8 dB from
the maximum value.
[0094] The optical transmitting device 80 according to the fifth embodiment monitors the
intensity of the modulation component of the optical frequency division multiplexed
signal, and converts the polarization state of the signal light beam at an angle of
90 degrees, in the case where the intensity of the modulation component is reduced
beyond 1.8 dB from the maximum value even though the polarization state of the signal
light beam fluctuates. As a result, a reduction in the intensity of the modulation
component caused by the polarization dependence of XPM can be reduced.
[0095] It is noted that the monitoring control unit 105 according to the fifth embodiment
converts the polarization state of the signal light beam at an angle of 90 degrees,
in the case where the intensity of the modulation component is reduced beyond 1.8
dB from the maximum value. However, the threshold at which the polarized light is
rotated is not limited to a point in time at which the intensity exceeds 1.8 dB from
the maximum value. Such a configuration may be possible in which the threshold is
set to a given point in time in the range in which the intensity is reduced by 4.8
dB beyond 1.8 dB from the maximum value and the polarization state of the signal light
beam is converted at an angle of 90 degrees.
[0096] Moreover, for the nonlinear medium 12 (12A, 12B, 12C, and 92) according to the embodiments,
an optical waveguide of high refractive index difference may be used such as an optical
fiber, a semiconductor optical amplifier, and a thin silicon waveguide, for example.
Particularly for the optical fiber, such a fiber and a waveguide may be adopted, including
a high nonlinear fiber in which germanium is doped in a core and a core diameter is
narrowed to improve a nonlinear coefficient, and in which germanium or bismuth, for
example, is doped in a core to improve a nonlinear refractive index. Furthermore,
such a fiber and a waveguide may be adopted, in which a mode field is reduced to improve
optical power density, a fiber and a waveguide using chalcogenide glass may be adopted,
or a fiber and a waveguide of photonic crystals may be adopted.
[0097] In addition, for the nonlinear medium 12 (12A, 12B, 12C, and 92) using other devices,
a semiconductor optical amplifier in a quantum well structure, a quantum dot semiconductor
optical amplifier, a silicon photonics waveguide or the like may be used. Moreover,
for the other nonlinear medium, such a device may be used that the secondary nonlinear
optical effect is generated such as a three-wave mixing device. In this case, such
a device may be used including a LiNbO
3 waveguide having a quasi phase matching structure, a GaAlAs device, and a secondary
nonlinear optical crystal, for example. It is noted that even in the case where a
secondary nonlinear optical medium is used, such a configuration is preferable in
which phase matching wavelength disposition is provided.
[0098] Moreover, the subcarrier modulation signal and the subcarrier modulation signal light
beam are also applicable to an amplitude modulation signal, a phase modulation signal,
a frequency modulation signal, a multilevel modulation signal, a frequency division
multiplexed signal, an orthogonal frequency division multiplexed (OFDM) signal, or
a quadrature amplitude modulation (QAM) signal, for example.
[0099] Furthermore, the components of the units illustrated in the drawings are not necessarily
physically configured as in the drawings. Namely, the specific forms of the distribution
and integration of the components are not limited to ones illustrated in the drawings.
All or a part of the components can be configured as functionally or physically distributed
or integrated in given units according to various loads, the use situations, or the
like.
[0100] In the disclosed mode, the polarization dependence of an all-optical modulator using
cross phase modulation can be reduced.
1. An optical frequency division multiplexer (1) comprising:
a nonlinear medium (11,12) that multiplexes, on a carrier light beam, a signal light
beam of a modulation signal that a carrier signal (fi) at a characteristic frequency
is modulated with an information signal (Bi), cross-phase-modulates the carrier light
beam with the signal light beam, frequency-multiplexes the information signal in the
signal light beam on the carrier light beam, generates an optical frequency division
multiplexed signal, and outputs the optical frequency division multiplexed signal;
and
a control unit (15,19) that controls a polarization state of the signal light beam
in a direction in which an intensity of a modulation component takes a maximum value,
based on the intensity of the modulation component involved in a modulation signal
at a desired characteristic frequency of the optical frequency division multiplexed
signal.
2. The optical frequency division multiplexer according to claim 1, wherein when the
intensity of the modulation component involved in the modulation signal at the desired
characteristic frequency of the optical frequency division multiplexed signal is reduced
beyond a predetermined threshold from a maximum value, the control unit controls the
polarization state of the signal light beam.
3. The optical frequency division multiplexer according to claim 1, wherein when the
intensity of the modulation component involved in the modulation signal at the desired
characteristic frequency of the optical frequency division multiplexed signal is reduced
beyond a predetermined threshold of 1.8 dB from a maximum value, the control unit
controls the polarization state of the signal light beam.
4. The optical frequency division multiplexer according to claim 2 or 3, wherein the
control unit (15A) includes:
an intensity converting unit (21) that converts a part of the optical frequency division
multiplexed signal into an intensity modulated signal;
an optoelectric conversion unit (22) that optoelectrically converts the converted
intensity modulated signal;
an extracting unit (23) that extracts the modulation component involved in the modulation
signal at the desired characteristic frequency of the optoelectrically converted intensity
modulated signal; and
an intensity detecting unit (24) that detects the intensity of the extracted modulation
component.
5. The optical frequency division multiplexer according to any one of claims 1 to 4,
wherein the control unit converts the polarization state of the signal light beam
at an angle of 90 degrees to make a relative angle between the polarization state
of the signal light beam and a polarization state of the carrier light beam within
an angle of 45 degrees.
6. The optical frequency division multiplexer (1B-1,1B-j) according to claim 1, wherein:
when the intensity of the modulation component involved in the modulation signal at
the desired characteristic frequency of the optical frequency division multiplexed
signal is reduced beyond a predetermined threshold from a maximum value, a receiving
device (3) that receives the optical frequency division multiplexed signal outputs
a control signal; and
when the control signal from the receiving device is detected, the control unit (19B)
controls the polarization state of the signal light beam.
7. The optical frequency division multiplexer according to claim 6, wherein when the
modulation component involved in the modulation signal at the desired characteristic
frequency is extracted in modulation components involved in modulation signals at
a plurality of characteristic frequencies of the optical frequency division multiplexed
signal, the optical frequency division multiplexed signal being cross-phase-modulated
at optical frequency division multiplexers, and the intensity of the modulation component
involved in the extracted modulation signal at the desired characteristic frequency
is reduced beyond the predetermined threshold, the receiving device (3) outputs the
control signal to the control unit of the optical frequency division multiplexer in
which cross phase modulation is performed with a signal light beam involved in the
modulation signal at the desired characteristic frequency.
8. The optical frequency division multiplexer according to claim 7, wherein the receiving
device (3) includes:
an intensity converting unit (41) that converts a part of the optical frequency division
multiplexed signal into an intensity modulated signal;
an optoelectric conversion unit (42) that optoelectrically converts the converted
intensity modulated signal;
a first extracting unit (44) that extracts the modulation component involved in modulation
signals at characteristic frequencies of optoelectrically converted intensity modulated
signals;
a second extracting unit (51) that extracts the modulation component involved in the
modulation signal at the desired characteristic frequency in a plurality of the extracted
modulation components; and
a detecting unit (51) that detects the intensity of the extracted modulation component.
9. The optical frequency division multiplexer according to any one of claims 6 to 8,
wherein the control unit (19B) converts the polarization state of the signal light
beam at an angle of 90 degrees to make a relative angle between the polarization state
of the signal light beam and a polarization state of the carrier light beam within
an angle of 45 degrees.
10. An optical frequency division multiplexer (1C) comprising:
a nonlinear medium (12C) that multiplexes, on a carrier light beam, a signal light
beam of a modulation signal that a carrier signal (fi) at a characteristic frequency
is modulated with an information signal (Bi), cross-phase-modulates the carrier light
beam with the signal light beam, frequency-multiplexes the information signal in the
signal light beam on the carrier light beam, generates an optical frequency division
multiplexed signal and outputs the optical frequency division multiplexed signal;
a polarization monitor (62) that extracts a part of the signal light beam and a part
of the carrier light beam multiplexed in a stage (11C) before an input to the nonlinear
medium and acquires a polarization state of the carrier light beam and a polarization
state of the signal light beam; and
a control unit (15C,19C) that controls the polarization state of the signal light
beam based on the polarization state of the carrier light beam acquired at the polarization
monitor.
11. The optical frequency division multiplexer according to claim 10, wherein when the
polarization state of the signal light beam is positioned on a hemisphere different
from a hemisphere on which the polarization state of the carrier light beam is positioned
using a Poincare sphere expressing the polarization state of the signal light beam
and the polarization state of the carrier light beam acquired at the polarization
monitor, the control unit controls the polarization state of the signal light beam
so that the polarization state of the signal light beam is positioned on a hemisphere
the same as a hemisphere on which the polarization state of the carrier light beam
is positioned.
12. The optical frequency division multiplexer according to claim 11, wherein when the
polarization state of the carrier light beam is circular polarization and the polarization
state of the signal light beam is linear polarization, the control unit converts the
polarization state of the signal light beam at an angle of 90 degrees so that the
polarization state of the signal light beam is positioned on a hemisphere the same
as a hemisphere on which the polarization state of the carrier light beam is positioned
when the polarization state of the signal light beam is positioned on a hemisphere
different from a hemisphere on which the polarization state of the carrier light beam
is positioned.
13. The optical frequency division multiplexer according to claim 11, wherein when the
polarization state of the carrier light beam and the polarization state of the signal
light beam are linear polarization, the control unit converts the polarization state
of the signal light beam at an angle of 90 degrees so that the polarization state
of the signal light beam is positioned on a hemisphere the same as a hemisphere on
which the polarization state of the carrier light beam is positioned when the polarization
state of the signal light beam is positioned on a hemisphere different from a hemisphere
on which the polarization state of the carrier light beam is positioned.
14. An optical frequency division multiplexer (80) comprising:
a plurality of optical transmission lines (74) individually disposed for signal light
beams of modulation signals that a carrier signal (fi) at a different characteristic
frequency is modulated with an information signal (Bi), the optical transmission lines
transmitting the signal light beams;
a plurality of polarization control units (82) individually disposed on the optical
transmission lines, the polarization control units controlling polarization states
of the signal light beams transmitted from the optical transmission lines;
a plurality of nonlinear medium (91,92) individually disposed on the polarization
control units, the nonlinear medium cross-phase-modulating a carrier light beam with
the signal light beams transmitted through the polarization control units, frequency-multiplexing
the information signal in the signal light beam on the carrier light beam, generating
an optical frequency division multiplexed signal and outputting the optical frequency
division multiplexed signal; and
a control unit (105) that monitors a modulation component involved in modulation signals
at characteristic frequencies in the optical frequency division multiplexed signal
and instructs the polarization control unit corresponding to a signal light beam of
a modulation signal involved in a characteristic frequency to control the polarization
state of the signal light beam in a direction in which an intensity of the modulation
component takes a maximum value for individual modulation components involved in the
modulation signals at the characteristic frequencies, when an intensity of the modulation
component involved in the characteristic frequency is reduced beyond a predetermined
threshold.
15. A polarization control method for an optical frequency division multiplexer (1), the
method causing the optical frequency division multiplexer to execute processes of:
multiplexing, on a carrier light beam, a signal light beam of a modulation signal
that a carrier signal (fi) at a characteristic frequency is modulated with an information
signal (Bi), cross-phase-modulating the carrier light beam with the signal light beam
through a nonlinear medium (12), and frequency-multiplexing the information signal
in the signal light beam on the carrier light beam to generate an optical frequency
division multiplexed signal; and
controlling a polarization state of the signal light beam in a direction in which
an intensity of a modulation component takes a maximum value, based on the intensity
of the modulation component involved in a modulation signal at a desired characteristic
frequency of the optical frequency division multiplexed signal.
16. A polarization control method for an optical frequency division multiplexer (1C),
the method causing the optical frequency division multiplexer to execute processes
of:
multiplexing, on a carrier light beam, a signal light beam of a modulation signal
that a carrier signal (fi) at a characteristic frequency is modulated with an information
signal (Bi), cross-phase-modulating the carrier light beam with the signal light beam
through a nonlinear medium (12C), and frequency-multiplexing the information signal
in the signal light beam on the carrier light beam to generate an optical frequency
division multiplexed signal;
extracting a part of the signal light beam and a part of the carrier light beam multiplexed
in a stage before an input to the nonlinear medium and acquiring a polarization state
of the carrier light beam and a polarization state of the signal light beam; and
controlling the polarization state of the signal light beam based on the acquired
polarization state of the carrier light beam.